Propulsion System (PS) for Nanosatellite Platform

    • Propulsion System (PS) for Nanosatellite Platform

    Purpose:
    Orbital maneuvering of cubesat-class spacecraft.
    Year of release: 2016
    Guaranteed service life (years): 3
    Estimated production / delivery time (months): 12
    Flight qualification of the product: No
    Possibility to adapt the product to customer requirements: Yes
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    Parameter Value
    Stock of characteristic velocity for nanosatellite with weight up to 5 kg up to 25-30 m/s
    The total mass of PS 1,3 kg
    Minimum energy consumption 3 - 5 W
    Maximum power consumption 12 W
    Working body weight up to 0,2 kg
    Supply voltage 5 - 12 V
    Preparation time for start of the PS (preheating) 60 s
    The maximum time of a single inclusion to generate thrust up to 1200 s
    Electrothermal engine thrust 0,003 - 0,01 N
    Overall dimensions 91 х 96 х 130 mm

    Description

    Electrothermal propulsion unit for nanosatellite platform.

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